Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K

 
PIIS086956520001377-7-1
DOI10.31857/S086956520001377-7
Publication type Article
Status Published
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Journal nameDoklady Akademii nauk
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Pages276-280
Abstract

  

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Received14.10.2018
Publication date16.10.2018
Number of characters368
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